|
gptkbp:instanceOf
|
jet engine
|
|
gptkbp:application
|
military training aircraft
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:diameter
|
0.9 m
|
|
gptkbp:engineType
|
axial
single-stage high-pressure turbine
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
annular
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 238
|
|
gptkbp:introduced
|
1970s
|
|
gptkbp:is_used_in
|
gptkb:Hawker_Siddeley_Hawk
|
|
gptkbp:length
|
1.8 m
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
gptkbp:number_of_stages
|
8
|
|
gptkbp:operational_status
|
gptkb:United_Arab_Emirates_Air_Force
gptkb:Indian_Air_Force
gptkb:Qatar_Emiri_Air_Force
gptkb:Royal_Air_Force
gptkb:Royal_Australian_Air_Force
gptkb:Royal_Navy
gptkb:Kuwaiti_Air_Force
gptkb:Omani_Air_Force
gptkb:South_African_Air_Force
gptkb:Saudi_Arabian_Air_Force
|
|
gptkbp:propulsion
|
3,500 lbf
|
|
gptkbp:related_to
|
gptkb:Rolls-Royce_Holdings
gptkb:Adour_Mk_951
gptkb:BAE_Systems
gptkb:Hawker_Siddeley_Hawk_200
engine performance
military training
aerospace engineering
aviation technology
military aviation
engine efficiency
jet propulsion
aircraft engines
turbofan engines
Hawker Siddeley Hawk 100
|
|
gptkbp:successor
|
gptkb:Adour_Mk_951
|
|
gptkbp:type
|
turbofan engine
|
|
gptkbp:weight
|
approximately 300 kg
|